TWI821323B - stage device - Google Patents
stage device Download PDFInfo
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- TWI821323B TWI821323B TW108123194A TW108123194A TWI821323B TW I821323 B TWI821323 B TW I821323B TW 108123194 A TW108123194 A TW 108123194A TW 108123194 A TW108123194 A TW 108123194A TW I821323 B TWI821323 B TW I821323B
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- Prior art keywords
- guide
- slider
- air
- axis direction
- stage device
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- 238000013461 design Methods 0.000 abstract description 6
- 238000012986 modification Methods 0.000 description 12
- 230000004048 modification Effects 0.000 description 12
- 238000005192 partition Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 3
- 239000000470 constituent Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000004590 computer program Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q1/00—Members which are comprised in the general build-up of a form of machine, particularly relatively large fixed members
- B23Q1/25—Movable or adjustable work or tool supports
- B23Q1/44—Movable or adjustable work or tool supports using particular mechanisms
- B23Q1/56—Movable or adjustable work or tool supports using particular mechanisms with sliding pairs only, the sliding pairs being the first two elements of the mechanism
- B23Q1/60—Movable or adjustable work or tool supports using particular mechanisms with sliding pairs only, the sliding pairs being the first two elements of the mechanism two sliding pairs only, the sliding pairs being the first two elements of the mechanism
- B23Q1/62—Movable or adjustable work or tool supports using particular mechanisms with sliding pairs only, the sliding pairs being the first two elements of the mechanism two sliding pairs only, the sliding pairs being the first two elements of the mechanism with perpendicular axes, e.g. cross-slides
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q5/00—Driving or feeding mechanisms; Control arrangements therefor
- B23Q5/22—Feeding members carrying tools or work
- B23Q5/26—Fluid-pressure drives
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/06—Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings
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- G—PHYSICS
- G12—INSTRUMENT DETAILS
- G12B—CONSTRUCTIONAL DETAILS OF INSTRUMENTS, OR COMPARABLE DETAILS OF OTHER APPARATUS, NOT OTHERWISE PROVIDED FOR
- G12B5/00—Adjusting position or attitude, e.g. level, of instruments or other apparatus, or of parts thereof; Compensating for the effects of tilting or acceleration, e.g. for optical apparatus
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/67—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
- H01L21/68—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere for positioning, orientation or alignment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/72—Sealings
- F16C33/74—Sealings of sliding-contact bearings
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Machine Tool Units (AREA)
- Container, Conveyance, Adherence, Positioning, Of Wafer (AREA)
- Details Of Measuring And Other Instruments (AREA)
- Physical Deposition Of Substances That Are Components Of Semiconductor Devices (AREA)
Abstract
本發明提供一種對象物不容易受熱的影響、並且設計自由度高之載台裝置。載台裝置(100)具備:空氣伺服驅動的滑動件(10);第1導件(12),引導滑動件(10)向第1方向的移動;致動器(14),向第2方向驅動第1導件(12);及第2導件(16),引導第1導件(12)向前述第2方向的移動。The present invention provides a stage device in which an object is not easily affected by heat and has a high degree of design freedom. The stage device (100) is provided with: an air servo-driven slider (10); a first guide (12) that guides the movement of the slider (10) in the first direction; and an actuator (14) that moves in the second direction. The first guide member (12) and the second guide member (16) are driven to guide the first guide member (12) to move in the second direction.
Description
本申請主張基於2018年8月30日申請之日本專利申請第2018-161393號的優先權。該申請的所有內容藉由參閱援用於本說明書中。 本發明有關一種載台裝置。This application claims priority based on Japanese Patent Application No. 2018-161393 filed on August 30, 2018. All contents of this application are incorporated by reference into this specification. The invention relates to a carrier device.
已知有用於在第1方向和與第1方向正交之第2方向將對象物進行定位之載台裝置。以往,提出有一種X軸方向及Y軸方向的導件各設有一個而被稱為堆疊型之載台裝置(例如專利文獻1)。 (先前技術文獻) (專利文獻) 專利文獻1:日本特開平5-57558號公報A stage device for positioning an object in a first direction and a second direction orthogonal to the first direction is known. Conventionally, a stage device called a stack type, in which one guide is provided in each of the X-axis direction and the Y-axis direction, has been proposed (for example, Patent Document 1). (prior technical literature) (patent document) Patent Document 1: Japanese Patent Application Publication No. 5-57558
(發明所欲解決之問題) 在專利文獻1中所記載之載台裝置中,藉由線性馬達驅動載台,因此,線性馬達的線圈所產生之熱可能會傳遞至載台以及載置於載台之對象物,使得對象物受熱的影響。 又,在載台裝置,當然還想要確保高設計自由度。 本發明係鑑於該種狀況而完成者,其目的在於提供一種對象物不容易受熱的影響,並且設計自由度高之載台裝置。 (解決問題之技術手段) 為了解決上述問題,本發明的一態樣的載台裝置,具備:空氣伺服驅動的滑動件;第1導件,引導滑動件向第1方向的移動;致動器,向第2方向驅動第1導件;及第2導件,引導第1導件向第2方向的移動。 另外,將以上構成要件的任意組合、本發明的構成要件及表現與裝置、方法、系統等之間進行相互替換亦有效作為本發明的態樣。 (發明之效果) 依本發明,能夠提供一種對象物不容易受熱的影響,並且設計自由度高之載台裝置。(The problem that the invention wants to solve) In the stage device described in Patent Document 1, the stage is driven by a linear motor. Therefore, the heat generated by the coil of the linear motor may be transferred to the stage and the object placed on the stage, causing the object to Affected by heat. In addition, of course, we also want to ensure a high degree of design freedom when installing on a stage. The present invention was made in view of this situation, and its object is to provide a stage device in which an object is not easily affected by heat and has a high degree of freedom in design. (Technical means to solve problems) In order to solve the above problem, a stage device according to one aspect of the present invention includes: an air servo-driven slider; a first guide that guides the movement of the slider in the first direction; and an actuator that drives the slider in the second direction. 1 guide member; and the 2nd guide member guides the movement of the 1st guide member in the second direction. In addition, any combination of the above constituent elements, and the mutual replacement of the constituent elements and expressions of the present invention with devices, methods, systems, etc. are also effective as aspects of the present invention. (The effect of the invention) According to the present invention, it is possible to provide a stage device in which an object is not easily affected by heat and has a high degree of freedom in design.
以下,對各圖式中所示之相同或相等的構成要件、構件、製程賦予相同的符號,並適當省略重複說明。又,為了便於理解,將各圖式中的構件的尺寸適當放大、縮小表示。又,在各圖式中對實施形態進行說明之基礎上省略並不重要之構件的一部分表示。 圖1係表示實施形態的載台裝置100之立體圖。為了方便說明,如圖示般設定如下XYZ座標系,亦即將第1導件12(後述)所延伸之第1方向設為X軸方向,將第2導件16(後述)所延伸之第2方向設為Y軸方向,將與兩者正交之方向設為Z軸方向。在本實施形態中,第1方向與第2方向正交,但並不限定與此。載台裝置100被稱為堆疊型的XY載台,且在X軸方向、Y軸方向將對象物進行定位。 載台裝置100具備:滑動件10、第1導件12、致動器14、兩個第2導件16、工作台18及控制部30(圖1中未圖示)。 以下,在Z軸方向上,相對於第2導件16將設置第1導件12之側作為上側而進行說明。 滑動件10如後述般,藉由空氣伺服驅動而向X軸方向驅動。第1導件12為在X軸方向上細長的長條狀構件,並且引導滑動件10向X軸方向的移動。致動器14將第1導件12向Y軸方向驅動。第2導件16引導第1導件12向Y軸方向的移動。 工作台18固定於滑動件10。於工作台18,例如,載置有半導體晶圓等的加工對象物等。使第1導件12向Y軸方向移動,使滑動件10向X軸方向移動,藉此能夠使工作台18向XY方向移動而在XY方向將對象物進行定位。 圖2係表示從與X軸方向正交之平面(亦即YZ平面)切斷之滑動件10及第1導件12的剖面。第1導件12包括底壁32、第1側壁34及第2側壁36。底壁32為在X軸方向較長之平板狀構件,且兩個主面以朝向Z軸方向之方式設置。第1側壁34為在X軸方向較長之立壁,且豎設於底壁32的上表面的Y軸方向上之另一端。第2側壁36與第1側壁34相同,為在X軸方向較長之立壁,且以與第1側壁34在Y軸方向相對向之方式豎設於底壁32的上表面的Y軸方向的另一端。第1側壁34、第2側壁36分別具有彼此相對向而延伸之第1延伸部34a、第2延伸部36a。因此,第1側壁34及第2側壁36具有L字形剖面形狀。 滑動件10為長方體狀構件,且收納於第1導件12的內側,亦即第1側壁34及第2側壁36與底壁32之間。在與第1導件12相對向之滑動件10的各面,亦即底面10a、第1側面10b、第2側面10c、上表面10d形成有一個或複數個氣墊40。氣墊40將從未圖示之供氣系統供給之高壓氣體噴出,而在其與第1導件12之間形成高壓氣體層。藉此,滑動件10保持微小的間隙而從第1導件12上浮。 在與第1側壁34相對向之第1側面10b、與第2側壁36相對向之第2側面10c形成有用於驅動滑動件10之空氣伺服室48。亦即,在本實施形態中,在滑動件10形成有兩個空氣伺服室48。藉此,能夠控制滑動件10繞Z軸旋轉。 在滑動件10的各面以包圍氣墊40之方式形成有差動排氣用排氣槽42、44、46。排氣槽42釋放於大氣。另外,排氣槽42亦可以與排氣泵(未圖示)連接。排氣槽44、46分別與用於將排氣槽內的壓力設為低真空壓力水準、中真空壓力水準之排氣泵(未圖示)連接,而將從滑動件10的氣墊40及空氣伺服室48向內部空間供給之壓縮氣體向外部排出。如此,避免壓縮氣體從第1導件12與滑動件10的間隙漏出,在真空環境下亦能夠使用載台裝置100。另外,當在大氣壓環境下使用載台裝置100時,無需設置該種排氣槽42、44、46。 圖3係圖2的A-A線剖面圖。參閱圖3,對滑動件10相對於第1導件12移動之原理進行說明。載台裝置100還具備兩個分隔壁56。在圖3中,將第1導件12與滑動件10的間隙或分隔壁56與空氣伺服室48之間隙誇大描繪。實際上,例如該等間隙為數微米左右。 分隔壁56固定於第1導件12,且在X軸方向將滑動件10的空氣伺服室48劃分為兩個空氣伺服室48A、48B。在兩個空氣伺服室48A、48B分別連接有用於使壓縮氣體能夠出入之供氣系統50A、50B。供氣系統50A、50B分別包括伺服閥52A、52B和壓縮氣體供給源54A、54B。 若對氣墊40供給壓縮氣體,則如上述,滑動件10相對於第1導件12稍微上浮。在該狀態下,例如對空氣伺服室48A供給壓縮氣體,並從空氣伺服室48B排出壓縮氣體,則分隔壁56作為活塞而發揮作用,使滑動件10向圖中的左方向移動。如此,藉由控制伺服閥52A、52B的開度,能夠相對於滑動件10使第1導件12移動到任意位置。 在此,滑動件10形成有兩個空氣伺服室48,且各空氣伺服室48連接有兩個供氣系統,亦即在滑動件10共連接有四個供氣系統,但並不限定於此。例如,可以將一個供氣系統50A分支而向兩個空氣伺服室48A供給壓縮氣體,將一個供氣系統50B分支而向兩個空氣伺服室48B供給壓縮氣體。又,例如,滑動件10可以僅形成有一個空氣伺服室48,且在將該空氣伺服室48劃分而成之空氣伺服室48A、48B連接有供氣系統50A、50B。亦即在滑動件10可以僅連接有共兩個供氣系統。 返回到圖1,第2導件16將第1導件12支撐成在Y軸方向上可移動自如。本實施形態中,兩個第2導件16設置在X軸方向上的致動器14的兩側,尤其設置成在X軸方向上與致動器14的距離相等。關於第2導件16,其構成並沒有特別限定,但在圖示的例子中為線性導件,包括:軌道24,向Y軸方向延伸;及滑塊26,固定於第1導件12的底壁32的下表面,並以支撐第1導件12之狀態在軌道24上行進。 圖4表示從與Y軸方向正交之平面(亦即XZ平面)切斷之載台裝置100的剖面。圖5係圖4的B-B線剖面圖。在圖5中,將固定體72與活動體70的間隙或分隔壁74與空氣伺服室80之間隙誇大描繪。實際上,例如該等間隙為數微米左右。 關於致動器14,其構成並沒有特別限定,但在圖示的例子中為空氣伺服致動器,包括活動體70、兩個固定體72及兩個分隔壁74。兩個固定體72為在Y軸方向較長之立壁,且在X軸方向隔開間隔地配置。活動體70為長方體狀的構件,且配置於兩個固定體72之間,並且被固定於第1導件12的底壁32的下表面。在與固定體72相對向之活動體70的各面,亦即在與一個固定體72相對向之第1側面70a及與另一個固定體72相對向之第2側面70b形成有用於驅動活動體之空氣伺服室80。 分隔壁74固定於固定體72,且在X軸方向將活動體70的空氣伺服室80劃分為兩個空氣伺服室80A、80B。在兩個空氣伺服室80A、80B分別連接有用於使壓縮氣體能夠出入之供氣系統90A、90B。供氣系統90A、90B分別包括伺服閥92A、92B和壓縮氣體供給源94A、94B。另外,活動體70以空氣伺服室80的內表面與分隔壁74成為非接觸之方式,亦即空氣伺服室80的內表面與分隔壁74之間存在間隙之方式透過第1導件12而被兩個第2導件16支撐。 例如,對空氣伺服室80A供給壓縮氣體,並從空氣伺服室80B排出壓縮氣體,則分隔壁74作為活塞而發揮作用,使活動體70向圖中的左方向移動。如此,藉由控制伺服閥92A、92B的開度,能夠使活動體70以及第1導件12向Y軸方向移動。 另外,在此活動體70形成有兩個空氣伺服室80,且各空氣伺服室80連接有兩個供氣系統,亦即在活動體70連接有共四個供氣系統,但並不限定於此。例如,可以將一個供氣系統90A分支而向兩個空氣伺服室80A供給壓縮氣體,將一個供氣系統90B分支而向兩個空氣伺服室80B供給壓縮氣體。又,例如,活動體70可以僅形成有一個空氣伺服室80,且在將該空氣伺服室80劃分而成之空氣伺服室80A、80B連接有供氣系統90A、90B。亦即在活動體70可以僅連接有共兩個供氣系統。 圖6係表示控制部30的功能及構造之方塊圖。關於在此所示之各方塊,在硬體方面,能夠藉由以電腦的CPU(central processing unit(中央處理器))為代表之元件或機械裝置而實現,在於軟體方面,可藉由電腦程式等而實現,但在此描繪有可藉該等的配合而實現之功能方塊。因此,本說明書中提及之本領域技術人員應當理解該等功能方塊能夠藉由硬體、軟體的組合而以各種形態實現之情況。 控制部30包括上浮控制部62及移動控制部64。上浮控制部62為了使滑動件10相對於第1導件12上浮而控制從氣墊40噴出之壓縮氣體的流量。移動控制部64為了使滑動件10移動而控制對空氣伺服室48供給之壓縮氣體的流量。又,移動控制部64為了使致動器14的活動體70的移動而控制對空氣伺服室80供給之壓縮氣體的流量。 接著,對本實施形態所發揮之效果進行描述。在此,例如,當滑動件10藉由線性馬達驅動時,線性馬達的線圈產生熱,其熱可能會傳遞至滑動件10、固定於滑動件10之工作台18、以及載置於工作台18之對象物。相對於此,本實施形態中,滑動件10藉由空氣伺服驅動。在該情況下,能夠使產生熱之壓縮氣體供給源54A、54B遠離滑動件10、工作台18,並能夠抑制其熱傳遞至滑動件10、工作台18。亦即,能夠降低傳遞至對象物之熱。另一方面,在致動器14與工作台18之間存在第1導件12,即便致動器14產生熱,其熱亦難以傳遞至工作台18、載置於工作台18之對象物。由此,本實施形態中,致動器14的構成並沒有特別限定,提高了設計的自由度。亦即,藉由本實施形態,能夠提供一種傳遞至對象物之熱被抑制,並且設計自由度高之載台裝置。 又,本實施形態中,兩個第2導件16設置於X軸方向上的致動器14的兩側。藉此,與第2導件16僅設置於X軸方向上的致動器14的一側的情況相比,能夠更穩定地將第1導件12支撐成在Y軸方向可移動自如。 以上,對實施形態之載台裝置進行說明。本領域技術人員應當理解該實施形態為例示,能夠對各構成要件的組合進行各種變形之情況,並且該種變形例亦屬於本發明的範圍內之情況。又,實施形態彼此還能夠進行組合。 (變形例1) 在實施形態中,對致動器14為空氣伺服致動器之情況進行了說明,但並不限定於此。致動器14只要能夠向Y軸方向驅動第1導件12即可,例如,可以為線性馬達,亦可以為音圈馬達,亦可以為旋轉型的馬達與滾珠螺桿進行組合者。 (變形例2) 實施形態中,對第2導件16為線性導件之情況進行了說明,但並不限定於此。 第2導件16可以為例如空氣導件。圖7係表示變形例的載台裝置100之剖面圖。圖7與圖4對應。在本變形例中,第2導件16包括:導軸124,向Y軸方向延伸;及筒狀的第2滑動件126,能夠以讓導軸124插穿之狀態沿導軸124移動。另外,在圖示的例子中,導軸124為長方體狀且第2滑動件126為方柱狀,但並不限定於此,例如,導軸124可以為圓柱狀且第2滑動件126可以為圓筒狀。 第2滑動件126對於導軸124具有微小的間隙,從設置於第2滑動件126的內部之氣墊(未圖示)噴出壓縮氣體,藉此使第2滑動件126能夠沿導軸124滑順地移動。 又,本變形例中,上浮控制部62進一步為了使第2滑動件126相對於導軸124上浮而控制從設置於第2滑動件126的內部之氣墊噴出之壓縮氣體的流量。 在此,若滑動件10沿第1導件12向X軸方向移動,則在第1導件12可能產生負載變動而使第1導件12繞Y軸方向傾斜,導致在致動器14的活動體70產生繞固定體72的轉矩。結果,會產生活動體70與固定體72接觸而引起之損傷。尤其,本變形例中,活動體70因氣體的壓力而上浮,因此若在活動體70產生繞固定體72之轉矩,則容易產生損傷。 於是,本變形例中,為了對於因滑動件10移動而可能於第1導件12產生之負載變動能得到足夠大的上浮剛性,換言之為了能夠抑制或防止負載變動所造成之第1導件12的沉入,上浮控制部62控制從設置於第2滑動件126的內部之氣墊噴出之氣體的流量。 具體而言,例如關於上浮控制部62,當滑動件10相對於致動器14移動至第1導件12的一側時,可以增加從這一側的第2導件16的第2滑動件126的氣墊噴出之氣體的流量,亦可以減少從另一側的第2導件16的第2滑動件126的氣墊噴出之氣體的流量或停止氣體的噴出,或者可以同時使用該等。相對於致動器14移動至第1導件12的另一側之情況亦相同。 (變形例3) 在實施形態中,對兩個第2導件16以相對於致動器14位於相反一側的方式固定於第1導件12之情況進行了說明,但並不限定於此,載台裝置100可以僅具備一個第2導件16,亦可以具備三個以上。 上述之實施形態與變形例的任意組合亦可作為本發明的實施形態而實用。藉由組合而產生之新的實施形態同時具有被組合之實施形態及變形例各自的效果。又,本領域技術人員應當理解申請專利範圍中所記載之各構成要件應發揮之功能可藉由在實施形態及變形例中所示之各構成要件的單體或該等的配合而實現之情況。In the following, the same or equivalent components, members, and processes shown in the drawings are given the same reference numerals, and repeated descriptions are appropriately omitted. In addition, in order to facilitate understanding, the dimensions of the members in each drawing are appropriately enlarged or reduced. In addition, in each drawing, the embodiment is described and a portion of the components that are not important are omitted. FIG. 1 is a perspective view of the stage device 100 according to the embodiment. For convenience of explanation, the following XYZ coordinate system is set as shown in the figure, that is, the first direction in which the first guide 12 (described later) extends is the X-axis direction, and the second direction in which the second guide 16 (described later) extends is The direction is set as the Y-axis direction, and the direction orthogonal to both is set as the Z-axis direction. In this embodiment, the first direction and the second direction are orthogonal to each other, but they are not limited to this. The stage device 100 is called a stacked XY stage, and positions an object in the X-axis direction and the Y-axis direction. The stage device 100 includes a slider 10, a first guide 12, an actuator 14, two second guides 16, a table 18, and a control unit 30 (not shown in FIG. 1 ). In the following description, the side where the first guide 12 is disposed is regarded as the upper side with respect to the second guide 16 in the Z-axis direction. As will be described later, the slider 10 is driven in the X-axis direction by air servo drive. The first guide 12 is an elongated member elongated in the X-axis direction and guides the movement of the slider 10 in the X-axis direction. The actuator 14 drives the first guide 12 in the Y-axis direction. The second guide 16 guides the movement of the first guide 12 in the Y-axis direction. The workbench 18 is fixed to the sliding member 10 . On the table 18, for example, a processing object such as a semiconductor wafer is placed. By moving the first guide 12 in the Y-axis direction and the slider 10 in the X-axis direction, the table 18 can be moved in the XY direction to position the object in the XY direction. FIG. 2 shows a cross-section of the slider 10 and the first guide 12 taken from a plane orthogonal to the X-axis direction (that is, the YZ plane). The first guide 12 includes a bottom wall 32 , a first side wall 34 and a second side wall 36 . The bottom wall 32 is a flat plate member that is long in the X-axis direction, and has two main surfaces facing the Z-axis direction. The first side wall 34 is a vertical wall that is longer in the X-axis direction and is erected on the other end of the upper surface of the bottom wall 32 in the Y-axis direction. The second side wall 36 is the same as the first side wall 34 in that it is a long vertical wall in the X-axis direction and is erected in the Y-axis direction on the upper surface of the bottom wall 32 in a manner opposite to the first side wall 34 in the Y-axis direction. another side. The first side wall 34 and the second side wall 36 respectively have a first extending portion 34a and a second extending portion 36a extending opposite to each other. Therefore, the first side wall 34 and the second side wall 36 have an L-shaped cross-sectional shape. The sliding member 10 is a rectangular parallelepiped-shaped member and is accommodated inside the first guide 12 , that is, between the first side wall 34 and the second side wall 36 and the bottom wall 32 . One or a plurality of air cushions 40 are formed on each surface of the slider 10 facing the first guide 12, that is, the bottom surface 10a, the first side surface 10b, the second side surface 10c, and the upper surface 10d. The air cushion 40 ejects high-pressure gas supplied from an air supply system (not shown) to form a high-pressure gas layer between the air cushion 40 and the first guide 12 . Thereby, the slider 10 floats up from the first guide 12 while maintaining a slight gap. An air servo chamber 48 for driving the slider 10 is formed on the first side 10b facing the first side wall 34 and the second side 10c facing the second side wall 36 . That is, in this embodiment, two air servo chambers 48 are formed in the slider 10 . Thereby, the slider 10 can be controlled to rotate around the Z-axis. Differential exhaust grooves 42 , 44 , and 46 are formed on each surface of the slider 10 so as to surround the air cushion 40 . The exhaust groove 42 releases air to the atmosphere. In addition, the exhaust tank 42 may also be connected to an exhaust pump (not shown). The exhaust grooves 44 and 46 are respectively connected to exhaust pumps (not shown) for setting the pressure in the exhaust groove to a low vacuum pressure level and a medium vacuum pressure level, and the air cushion 40 and air from the sliding member 10 are The compressed gas supplied to the internal space of the servo chamber 48 is discharged to the outside. In this way, the compressed gas is prevented from leaking from the gap between the first guide 12 and the sliding member 10, and the stage device 100 can be used in a vacuum environment. In addition, when the stage device 100 is used in an atmospheric pressure environment, there is no need to provide such exhaust grooves 42, 44, and 46. Figure 3 is a cross-sectional view along line A-A in Figure 2 . Referring to FIG. 3 , the principle of movement of the sliding member 10 relative to the first guide member 12 will be described. The stage device 100 further includes two partition walls 56 . In FIG. 3 , the gap between the first guide 12 and the slider 10 or the gap between the partition wall 56 and the air servo chamber 48 is exaggerated. In practice, these gaps are, for example, on the order of several microns. The partition wall 56 is fixed to the first guide 12 and divides the air servo chamber 48 of the slider 10 into two air servo chambers 48A and 48B in the X-axis direction. The two air servo chambers 48A and 48B are respectively connected to air supply systems 50A and 50B for allowing compressed gas to enter and exit. The gas supply systems 50A and 50B respectively include servo valves 52A and 52B and compressed gas supply sources 54A and 54B. When compressed air is supplied to the air cushion 40 , the slider 10 floats slightly relative to the first guide 12 as described above. In this state, for example, if compressed gas is supplied to the air servo chamber 48A and the compressed gas is discharged from the air servo chamber 48B, the partition wall 56 functions as a piston and moves the slider 10 to the left in the figure. In this way, by controlling the opening of the servo valves 52A and 52B, the first guide 12 can be moved to an arbitrary position relative to the slider 10 . Here, the sliding member 10 is formed with two air servo chambers 48, and each air servo chamber 48 is connected to two air supply systems. That is, a total of four air supply systems are connected to the sliding member 10, but it is not limited to this. . For example, one air supply system 50A may be branched to supply compressed gas to two air servo chambers 48A, and one air supply system 50B may be branched to supply compressed gas to two air servo chambers 48B. Furthermore, for example, the slider 10 may be formed with only one air servo chamber 48, and the air supply systems 50A and 50B may be connected to the air servo chambers 48A and 48B that divide the air servo chamber 48. That is to say, only two air supply systems can be connected to the sliding member 10 . Returning to FIG. 1 , the second guide 16 supports the first guide 12 movably in the Y-axis direction. In this embodiment, the two second guides 16 are provided on both sides of the actuator 14 in the X-axis direction, and particularly are provided at an equal distance from the actuator 14 in the X-axis direction. The structure of the second guide 16 is not particularly limited, but in the example shown in the figure, it is a linear guide, including: a rail 24 extending in the Y-axis direction; and a slider 26 fixed to the first guide 12 The lower surface of the bottom wall 32 travels on the rail 24 while supporting the first guide 12 . FIG. 4 shows a cross-section of the stage device 100 cut from a plane orthogonal to the Y-axis direction (that is, the XZ plane). Figure 5 is a cross-sectional view taken along line B-B in Figure 4 . In FIG. 5 , the gap between the fixed body 72 and the movable body 70 or the gap between the partition wall 74 and the air servo chamber 80 is exaggeratedly drawn. In practice, these gaps are, for example, on the order of several microns. The structure of the actuator 14 is not particularly limited, but in the example shown in the figure, it is an air servo actuator and includes a movable body 70 , two fixed bodies 72 and two partition walls 74 . The two fixed bodies 72 are vertical walls that are long in the Y-axis direction and are arranged at intervals in the X-axis direction. The movable body 70 is a rectangular parallelepiped-shaped member, is arranged between the two fixed bodies 72 , and is fixed to the lower surface of the bottom wall 32 of the first guide 12 . On each side of the movable body 70 facing the fixed body 72 , that is, on the first side 70 a facing the one fixed body 72 and the second side 70 b facing the other fixed body 72 , there are formed holes for driving the movable body. The air servo chamber 80. The partition wall 74 is fixed to the fixed body 72 and divides the air servo chamber 80 of the movable body 70 into two air servo chambers 80A and 80B in the X-axis direction. The two air servo chambers 80A and 80B are respectively connected to air supply systems 90A and 90B for allowing compressed gas to enter and exit. Gas supply systems 90A, 90B include servo valves 92A, 92B and compressed gas supply sources 94A, 94B, respectively. In addition, the movable body 70 is moved through the first guide 12 in such a manner that the inner surface of the air servo chamber 80 and the partition wall 74 are in non-contact, that is, there is a gap between the inner surface of the air servo chamber 80 and the partition wall 74 . Two second guides 16 support. For example, when compressed gas is supplied to the air servo chamber 80A and the compressed gas is discharged from the air servo chamber 80B, the partition wall 74 functions as a piston and moves the movable body 70 to the left direction in the figure. In this way, by controlling the opening of the servo valves 92A and 92B, the movable body 70 and the first guide 12 can be moved in the Y-axis direction. In addition, two air servo chambers 80 are formed in the movable body 70 , and each air servo chamber 80 is connected to two air supply systems. That is, a total of four air supply systems are connected to the movable body 70 . However, this is not limited to this. For example, one air supply system 90A may be branched to supply compressed gas to two air servo chambers 80A, and one air supply system 90B may be branched to supply compressed gas to two air servo chambers 80B. Furthermore, for example, the movable body 70 may be formed with only one air servo chamber 80 , and the air supply systems 90A and 90B may be connected to the air servo chambers 80A and 80B that divide the air servo chamber 80 . That is, only a total of two air supply systems may be connected to the movable body 70 . FIG. 6 is a block diagram showing the function and structure of the control unit 30. Regarding the blocks shown here, in terms of hardware, they can be implemented by components or mechanical devices represented by a computer's CPU (central processing unit), and in terms of software, they can be implemented by computer programs. etc., but here are functional blocks that can be realized by the cooperation of these. Therefore, those skilled in the art mentioned in this specification should understand that these functional blocks can be implemented in various forms through a combination of hardware and software. The control unit 30 includes a floating control unit 62 and a movement control unit 64 . The floating control unit 62 controls the flow rate of the compressed gas ejected from the air cushion 40 in order to float the slider 10 relative to the first guide 12 . The movement control unit 64 controls the flow rate of the compressed gas supplied to the air servo chamber 48 in order to move the slider 10 . Furthermore, the movement control unit 64 controls the flow rate of the compressed gas supplied to the air servo chamber 80 in order to move the movable body 70 of the actuator 14 . Next, the effects exerted by this embodiment will be described. Here, for example, when the slider 10 is driven by a linear motor, the coil of the linear motor generates heat, and the heat may be transferred to the slider 10 , the workbench 18 fixed to the slider 10 , and the workbench 18 object. On the other hand, in this embodiment, the slider 10 is servo-driven by air. In this case, the compressed gas supply sources 54A and 54B that generate heat can be kept away from the slider 10 and the table 18, and the heat transfer to the slider 10 and the table 18 can be suppressed. That is, the heat transferred to the object can be reduced. On the other hand, since the first guide 12 is present between the actuator 14 and the table 18 , even if the actuator 14 generates heat, the heat is difficult to be transferred to the table 18 or the object placed on the table 18 . Therefore, in this embodiment, the structure of the actuator 14 is not particularly limited, thereby increasing the degree of freedom in design. That is, according to this embodiment, it is possible to provide a stage device in which the heat transmitted to the object is suppressed and the design freedom is high. Furthermore, in this embodiment, two second guides 16 are provided on both sides of the actuator 14 in the X-axis direction. Thereby, compared with the case where the second guide 16 is provided only on one side of the actuator 14 in the X-axis direction, the first guide 12 can be supported movably in the Y-axis direction more stably. The stage device according to the embodiment has been described above. Those skilled in the art will understand that this embodiment is only an example and that various modifications can be made to the combination of each component, and such modifications are also within the scope of the present invention. Furthermore, the embodiments can be combined with each other. (Modification 1) In the embodiment, the case where the actuator 14 is an air servo actuator has been described, but the invention is not limited to this. The actuator 14 only needs to be able to drive the first guide 12 in the Y-axis direction. For example, it may be a linear motor, a voice coil motor, or a combination of a rotary motor and a ball screw. (Modification 2) In the embodiment, the case where the second guide 16 is a linear guide has been described, but the invention is not limited to this. The second guide 16 may be an air guide, for example. FIG. 7 is a cross-sectional view showing a stage device 100 according to a modified example. Figure 7 corresponds to Figure 4. In this modification, the second guide 16 includes a guide shaft 124 extending in the Y-axis direction, and a cylindrical second slider 126 capable of moving along the guide shaft 124 with the guide shaft 124 inserted therethrough. In addition, in the example shown in the figure, the guide shaft 124 is in the shape of a rectangular parallelepiped and the second slider 126 is in the shape of a square column. However, it is not limited thereto. For example, the guide shaft 124 may be in a cylindrical shape and the second slider 126 may be in a cylindrical shape. Cylindrical shape. The second sliding member 126 has a slight gap with respect to the guide shaft 124, and compressed air is ejected from an air cushion (not shown) provided inside the second sliding member 126, thereby allowing the second sliding member 126 to slide smoothly along the guide shaft 124. move. Furthermore, in this modification, the floating control unit 62 further controls the flow rate of the compressed gas ejected from the air cushion provided inside the second slider 126 in order to float the second slider 126 relative to the guide shaft 124 . Here, if the slider 10 moves in the X-axis direction along the first guide 12, a load change may occur on the first guide 12, causing the first guide 12 to tilt around the Y-axis direction, causing the actuator 14 to move in the direction of the Y-axis. The movable body 70 generates a torque around the fixed body 72 . As a result, damage may occur due to contact between the movable body 70 and the fixed body 72 . In particular, in this modification, the movable body 70 floats due to the pressure of the gas. Therefore, if a torque around the fixed body 72 is generated in the movable body 70, damage may easily occur. Therefore, in this modification, in order to obtain sufficient floating rigidity against the load variation that may occur on the first guide 12 due to the movement of the slider 10 , in other words, in order to suppress or prevent the first guide 12 from being caused by the load variation. The sinking and rising control unit 62 controls the flow rate of the gas ejected from the air cushion provided inside the second slider 126 . Specifically, for example, regarding the floating control portion 62 , when the slider 10 moves to one side of the first guide 12 relative to the actuator 14 , the second slider of the second guide 16 from this side can be added. The flow rate of the gas ejected from the air cushion 126 can also be reduced or the gas ejection stopped from the air cushion of the second slider 126 of the second guide 16 on the other side, or these can be used simultaneously. The same is true when the actuator 14 moves to the other side of the first guide 12 . (Modification 3) In the embodiment, the case where the two second guides 16 are fixed to the first guide 12 so as to be located on the opposite side with respect to the actuator 14 has been described. However, the present invention is not limited to this. The stage device 100 Only one second guide 16 may be provided, or three or more second guides 16 may be provided. Any combination of the above-described embodiments and modifications can also be put into practical use as an embodiment of the present invention. A new embodiment produced by combination has the respective effects of the combined embodiments and modifications. In addition, those skilled in the art will understand that the functions to be performed by each component described in the claimed scope can be realized by a single component of each component shown in the embodiments and modifications or by a combination thereof. .
10‧‧‧滑動件 12‧‧‧第1導件 14‧‧‧致動器 16‧‧‧第2導件 100‧‧‧載台裝置10‧‧‧Sliding parts 12‧‧‧1st Guide 14‧‧‧Actuator 16‧‧‧2nd guide 100‧‧‧Carrying device
圖1係表示實施形態的載台裝置之立體圖。 圖2係表示圖1的X軸導件及X軸滑動件的剖面之圖。 圖3係圖2的A-A線剖面圖。 圖4係表示圖1的載台裝置的剖面之圖。 圖5係圖4的B-B線剖面圖。 圖6係表示控制部的功能及構造之方塊圖。 圖7係表示變形例的載台裝置之剖面圖。FIG. 1 is a perspective view of the stage device according to the embodiment. FIG. 2 is a cross-sectional view showing the X-axis guide and the X-axis slider of FIG. 1 . Figure 3 is a cross-sectional view along line A-A in Figure 2 . FIG. 4 is a cross-sectional view of the stage device of FIG. 1 . Figure 5 is a cross-sectional view taken along line B-B in Figure 4 . FIG. 6 is a block diagram showing the function and structure of the control unit. FIG. 7 is a cross-sectional view showing a modified example of the stage device.
10‧‧‧引導滑動件 10‧‧‧Guide slide
12‧‧‧第1導件 12‧‧‧1st Guide
14‧‧‧致動器 14‧‧‧Actuator
16‧‧‧第2導件 16‧‧‧2nd guide
18‧‧‧工作台 18‧‧‧Workbench
24‧‧‧軌道 24‧‧‧Track
26‧‧‧滑塊 26‧‧‧Slider
32‧‧‧底壁 32‧‧‧Bottom wall
70‧‧‧活動體 70‧‧‧Mobile objects
72‧‧‧固定體 72‧‧‧Fixed body
74‧‧‧分隔壁 74‧‧‧Partition Wall
80‧‧‧空氣伺服室 80‧‧‧Air servo room
100‧‧‧載台裝置 100‧‧‧Carrying device
Claims (3)
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JP2018161393 | 2018-08-30 | ||
JP2018-161393 | 2018-08-30 |
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TW202009094A TW202009094A (en) | 2020-03-01 |
TWI821323B true TWI821323B (en) | 2023-11-11 |
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TW108123194A TWI821323B (en) | 2018-08-30 | 2019-07-02 | stage device |
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JP (1) | JP7328975B2 (en) |
TW (1) | TWI821323B (en) |
WO (1) | WO2020044685A1 (en) |
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TWI806474B (en) * | 2021-04-01 | 2023-06-21 | 日商住友重機械工業股份有限公司 | Table device, exposure device, inspection device, and device manufacturing method |
WO2024190524A1 (en) * | 2023-03-13 | 2024-09-19 | 住友重機械工業株式会社 | Gas pressure driving device, positioning device, processing device, and device manufacturing method |
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TW200607211A (en) * | 2004-07-12 | 2006-02-16 | Sumitomo Heavy Industries | Linear motor and stage arrangement employing the linear motor |
TW200724294A (en) * | 2005-12-22 | 2007-07-01 | Ushio Electric Inc | Planar carrying stage device |
TW200740550A (en) * | 2006-03-02 | 2007-11-01 | Sumitomo Heavy Industries | Stage apparatus |
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TW201813758A (en) * | 2016-10-13 | 2018-04-16 | 住友重機械工業股份有限公司 | Stage device |
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JP3687362B2 (en) * | 1998-03-31 | 2005-08-24 | 日本精工株式会社 | 2-axis moving device |
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JP2004319902A (en) * | 2003-04-18 | 2004-11-11 | Advantest Corp | Stage device and exposure device |
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- 2019-05-27 WO PCT/JP2019/020883 patent/WO2020044685A1/en active Application Filing
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- 2019-07-02 TW TW108123194A patent/TWI821323B/en active
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TW200607211A (en) * | 2004-07-12 | 2006-02-16 | Sumitomo Heavy Industries | Linear motor and stage arrangement employing the linear motor |
TW200724294A (en) * | 2005-12-22 | 2007-07-01 | Ushio Electric Inc | Planar carrying stage device |
TW200740550A (en) * | 2006-03-02 | 2007-11-01 | Sumitomo Heavy Industries | Stage apparatus |
TW200940235A (en) * | 2008-03-31 | 2009-10-01 | Sumitomo Heavy Industries | XY stage device |
TW201431631A (en) * | 2013-02-04 | 2014-08-16 | Shuz Tung Machinery Ind Co Ltd | Laser cut apparatus |
TW201813758A (en) * | 2016-10-13 | 2018-04-16 | 住友重機械工業股份有限公司 | Stage device |
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JP7328975B2 (en) | 2023-08-17 |
JPWO2020044685A1 (en) | 2021-09-09 |
WO2020044685A1 (en) | 2020-03-05 |
TW202009094A (en) | 2020-03-01 |
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